EP3009352A1 - Elektrothermisches nanosat-entfaltungssystem - Google Patents

Elektrothermisches nanosat-entfaltungssystem Download PDF

Info

Publication number
EP3009352A1
EP3009352A1 EP15182110.5A EP15182110A EP3009352A1 EP 3009352 A1 EP3009352 A1 EP 3009352A1 EP 15182110 A EP15182110 A EP 15182110A EP 3009352 A1 EP3009352 A1 EP 3009352A1
Authority
EP
European Patent Office
Prior art keywords
fusible line
secured
electroconductive material
fusible
nanosat
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP15182110.5A
Other languages
English (en)
French (fr)
Other versions
EP3009352B1 (de
Inventor
Geoffrey Orias
Michael Worcester
John Behrens
Bruce L. Drolen
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Boeing Co
Original Assignee
Boeing Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Boeing Co filed Critical Boeing Co
Publication of EP3009352A1 publication Critical patent/EP3009352A1/de
Application granted granted Critical
Publication of EP3009352B1 publication Critical patent/EP3009352B1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/66—Arrangements or adaptations of apparatus or instruments, not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/645—Separators
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/222—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/222—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state
    • B64G1/2229—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state characterised by the deployment actuating mechanism
    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B3/00—Ohmic-resistance heating
    • H05B3/0014—Devices wherein the heating current flows through particular resistances
    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B3/00—Ohmic-resistance heating
    • H05B3/02—Details
    • H05B3/06—Heater elements structurally combined with coupling elements or holders
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/222—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state
    • B64G1/2221—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state characterised by the manner of deployment
    • B64G1/2222—Folding

Definitions

  • An electrical wiring harness 48 is secured to the burn bar 42 as shown.
  • a positive electrical lead 50 and a negative electrical lead 52 have their respective ends 54, 56 secured to opposed sides of the burn bar 42, more specifically to lead connection structures 58.
  • a fusible line 60 is secured tightly across the burn bar 42, and specifically at a position to make direct contact with the resistor pad 44.
  • the fusible line 60 as shown and described herein is a single strand or monofilament. Such fusible line 60 may alternatively consist of a multi-strand line in appropriate scenarios, e.g. one requiring higher load-bearing, for example.
  • An electrical source 36 (shown schematically in FIG.
  • the substrate body 46 of the burn bar 42 may be formed of an aluminum alloy.
  • the burn bar 42 may be formed as part of a printed circuit board, and may be approximately 80 thousandths of an inch diameter, and configured to satisfactorily handle 12 volts without failure for achieving reliable and satisfactory electrothermal deployment.
  • the positive and negative lead lines 50, 52 may each be of 30 gauge thickness, and may be formed of copper metal.
  • FIG. 5A displays a second embodiment of a deployment device 140, which includes a resistive element 142 formed of a straight solid cylindrical substrate body 146, as depicted. However, the fusible line 160 of the deployment device 140 passes through a U-clamp line guide 180.

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Photovoltaic Devices (AREA)
  • Fuses (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Control Of Resistance Heating (AREA)
EP15182110.5A 2014-10-17 2015-08-24 Elektrothermisches nanosat-entfaltungssystem Active EP3009352B1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US14/517,532 US9446864B2 (en) 2014-10-17 2014-10-17 NANOSAT electrothermal deployment system

Publications (2)

Publication Number Publication Date
EP3009352A1 true EP3009352A1 (de) 2016-04-20
EP3009352B1 EP3009352B1 (de) 2019-12-25

Family

ID=54007560

Family Applications (1)

Application Number Title Priority Date Filing Date
EP15182110.5A Active EP3009352B1 (de) 2014-10-17 2015-08-24 Elektrothermisches nanosat-entfaltungssystem

Country Status (6)

Country Link
US (1) US9446864B2 (de)
EP (1) EP3009352B1 (de)
JP (1) JP6745590B2 (de)
KR (1) KR102435931B1 (de)
CN (1) CN105523199B (de)
BR (1) BR102015024262B1 (de)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2551880A (en) * 2016-05-03 2018-01-03 Harris Corp Payload deployment system
US20220396371A1 (en) * 2021-06-10 2022-12-15 The Boeing Company Apparatus for restraining an aircraft
US11712834B2 (en) 2017-11-29 2023-08-01 Eugen Seitz Ag Valve unit

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11148834B2 (en) 2017-11-10 2021-10-19 Spire Global, Inc. Systems and methods for satellite solar panel stowage and deployment
US11148831B2 (en) 2017-11-10 2021-10-19 Spire Global, Inc. Systems and methods for satellite solar panel deployment
US10676217B2 (en) * 2017-11-10 2020-06-09 Spire Global, Inc. Deployable satellite solar panel hinge mechanism
US10926891B2 (en) 2017-11-10 2021-02-23 Spire Global, Inc. Hold down and release mechanism for a deployable satellite solar panel
KR102084710B1 (ko) * 2018-06-01 2020-03-04 조선대학교산학협력단 포고핀을 이용한 큐브위성용 전개구조물 분리장치
KR102114295B1 (ko) * 2018-10-17 2020-05-22 조선대학교산학협력단 다축 구속이 가능한 큐브 위성용 전개구조물 구속/분리 장치
JP7284987B2 (ja) * 2019-04-24 2023-06-01 山田技研株式会社 人工衛星に搭載するアンテナ
US12006071B1 (en) * 2021-03-04 2024-06-11 Government Of The United States As Represented By The Secretary Of The Air Force Deployable radiator panel system
CN116654290A (zh) * 2021-04-23 2023-08-29 中国科学院微小卫星创新研究院 一种使用弹性热刀解锁装置解锁星上部件的方法
CN113479349B (zh) * 2021-04-25 2023-02-28 上海空间电源研究所 一种卫星用太阳帆板展开电路
CN113753266A (zh) * 2021-09-23 2021-12-07 北京国电高科科技有限公司 熔线式压紧释放装置

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2001055663A2 (en) * 2000-01-28 2001-08-02 Lockheed Martin Corporation Separation system for missile payload fairings
EP1612141A1 (de) * 2004-07-01 2006-01-04 EADS Space Transportation GmbH Vorrichtung zur lösbaren Halterung von Bauteilen
US8006936B1 (en) * 2006-05-31 2011-08-30 Farr Iii Warren W Parachute deployment control

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN100345728C (zh) * 2005-10-21 2007-10-31 哈尔滨工业大学 桁架式可刚化充气展开的太阳电池阵
US8033684B2 (en) 2007-08-31 2011-10-11 The Boeing Company Starry sky lighting panels
US8886388B2 (en) 2009-06-29 2014-11-11 The Boeing Company Embedded damage detection system for composite materials of an aircraft
US8745864B2 (en) 2009-08-10 2014-06-10 The Boeing Company Method of coupling digitizing sensors to a structure
FR2952353B1 (fr) * 2009-11-10 2011-12-09 Thales Sa Systeme de tirant actif permettant le maintien et la liberation sans choc d'appendices spatiaux
US8766511B2 (en) 2011-08-17 2014-07-01 The Boeing Company Method and system for distributed network of nanoparticle ink based piezoelectric sensors for structural health monitoring
US9127597B2 (en) 2011-09-23 2015-09-08 The Boeing Company Sensor system
WO2013049588A1 (en) * 2011-09-29 2013-04-04 The Government Of The United States Of America, As Represented By The Secretary Of The Navy Tethered spacecraft and separation system for tethered spacecraft

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2001055663A2 (en) * 2000-01-28 2001-08-02 Lockheed Martin Corporation Separation system for missile payload fairings
EP1612141A1 (de) * 2004-07-01 2006-01-04 EADS Space Transportation GmbH Vorrichtung zur lösbaren Halterung von Bauteilen
US8006936B1 (en) * 2006-05-31 2011-08-30 Farr Iii Warren W Parachute deployment control

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
ALPHONSO STEWART ET AL: "Intricacies of Using Kevlar Cord and Thermal Knives in a Deployable Release System: Issues and Solutions", PROCEEDINGS OF THE 36TH AEROSPACE MECHANISMS SYMPSOIUM, GLENN RESEARCH CENTER, MAY 15-17, 2002, 17 May 2002 (2002-05-17), XP055253404 *
J BOUWMEESTER ET AL: "PRELIMINARY MISSION RESULTS AND PROJECT EVALUATION OF THE DELFI-C 3 NANO-SATELLITE", PROCEEDINGS OF 4S SYMPOSIUM, NO. 1. 2008, GREECE, 1 June 2008 (2008-06-01), XP055253394, Retrieved from the Internet <URL:http://www.lr.tudelft.nl/fileadmin/Faculteit/LR/Organisatie/Afdelingen_en_Leerstoelen/Afdeling_SpE/Space_Systems_Eng./Publications/2008/doc/4S_2008,_Mission_Results_and_Project_Evaluation_of_Delfi-C3.pdf> [retrieved on 20160226] *

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2551880A (en) * 2016-05-03 2018-01-03 Harris Corp Payload deployment system
GB2551880B (en) * 2016-05-03 2018-06-20 Harris Corp Payload deployment system
US11712834B2 (en) 2017-11-29 2023-08-01 Eugen Seitz Ag Valve unit
US20220396371A1 (en) * 2021-06-10 2022-12-15 The Boeing Company Apparatus for restraining an aircraft
US11858658B2 (en) * 2021-06-10 2024-01-02 The Boeing Company Apparatus for restraining an aircraft

Also Published As

Publication number Publication date
CN105523199A (zh) 2016-04-27
JP6745590B2 (ja) 2020-08-26
CN105523199B (zh) 2020-01-21
BR102015024262A2 (pt) 2016-04-19
EP3009352B1 (de) 2019-12-25
JP2016078833A (ja) 2016-05-16
US9446864B2 (en) 2016-09-20
US20160107771A1 (en) 2016-04-21
BR102015024262B1 (pt) 2021-08-03
KR20160046304A (ko) 2016-04-28
KR102435931B1 (ko) 2022-08-23

Similar Documents

Publication Publication Date Title
EP3009352B1 (de) Elektrothermisches nanosat-entfaltungssystem
US5046426A (en) Sequential structural separation system
Hodges et al. A Deployable High-Gain Antenna Bound for Mars: Developing a new folded-panel reflectarray for the first CubeSat mission to Mars
US10351269B2 (en) Burn wire release mechanism for spacecraft and terrestrial applications
EP2882649B1 (de) Kleinvolumiger mikrosatellit mit flexiblen gewickelten, nach dem abschuss expandierbaren platten
JP7279884B2 (ja) 宇宙機、装置、及び、宇宙器を軌道離脱させる方法
US10689134B2 (en) Device for controlled separation between two parts and use of such a device
US6357699B1 (en) Device for controlled release of tension
Park et al. Development of 6 U CubeSat’s deployable solar panel with burn wire triggering holding and release mechanism
US6439122B1 (en) Separation system for missile payload fairings
Sureda et al. Design and testing of a helix antenna deployment system for a 1U CubeSat
US10443648B2 (en) Hinge assembly for a space structure
US11858658B2 (en) Apparatus for restraining an aircraft
KR102266285B1 (ko) 로버 착륙 장치 및 착륙선
US20220396377A1 (en) Method and device for deorbiting an artificial satellite from earth orbit
Laurin Development of Deployable Antennas for Advanced Maritime Communication and Monitoring withSmall Satellites
Sakamoto et al. Space demonstration of two-layer deployable membrane reflectarray antenna with popup book mechanism
US20240117795A1 (en) Integrated planar sma device and method
JPH09315399A (ja) ワイヤ保持解放装置
US10815011B2 (en) Restraint system for deployment of a feature on a satellite
Koo et al. Hot Firing Test of a Quadrature NEA SSD9103S1 Configuration
Kobza Space Qualification Testing of a Deployable Shape Memory Alloy CubeSat Antenna
Clark et al. Design of a Representative Low Earth Orbit Satellite to Improve Existing Debris Models
Hernandez Jr Non-Metallic Hold Down and Release for an RF Antenna

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20150824

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: EXAMINATION IS IN PROGRESS

17Q First examination report despatched

Effective date: 20181029

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

RIC1 Information provided on ipc code assigned before grant

Ipc: B64G 1/22 20060101AFI20190430BHEP

Ipc: H05B 3/00 20060101ALI20190430BHEP

Ipc: H05B 3/06 20060101ALI20190430BHEP

INTG Intention to grant announced

Effective date: 20190528

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAJ Information related to disapproval of communication of intention to grant by the applicant or resumption of examination proceedings by the epo deleted

Free format text: ORIGINAL CODE: EPIDOSDIGR1

GRAL Information related to payment of fee for publishing/printing deleted

Free format text: ORIGINAL CODE: EPIDOSDIGR3

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: EXAMINATION IS IN PROGRESS

GRAR Information related to intention to grant a patent recorded

Free format text: ORIGINAL CODE: EPIDOSNIGR71

INTC Intention to grant announced (deleted)
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

INTG Intention to grant announced

Effective date: 20191113

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 1216852

Country of ref document: AT

Kind code of ref document: T

Effective date: 20200115

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602015044170

Country of ref document: DE

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20191225

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20191225

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200325

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20191225

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20191225

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200325

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20191225

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200326

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20191225

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20191225

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20191225

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20191225

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20191225

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200520

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20191225

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20191225

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200425

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20191225

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20191225

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602015044170

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20191225

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20191225

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 1216852

Country of ref document: AT

Kind code of ref document: T

Effective date: 20191225

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20191225

26N No opposition filed

Effective date: 20200928

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20191225

Ref country code: IT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20191225

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20191225

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20191225

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200831

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200824

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200831

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20200831

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200824

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200831

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20191225

Ref country code: MT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20191225

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20191225

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20191225

P01 Opt-out of the competence of the unified patent court (upc) registered

Effective date: 20230516

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20230828

Year of fee payment: 9

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20230825

Year of fee payment: 9

Ref country code: DE

Payment date: 20230829

Year of fee payment: 9